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Numerical investigation on vortex-induced vibrations of four circular cylinders in a square configuration

机译:正方形结构中四个圆柱的涡激振动数值研究

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This paper presents a numerical study of two-degree-of-freedom vortex-induced vibration of four elastically mounted circular cylinders in a square arrangement at a low Reynolds number of Re = 150 and mass ratio of 2.0. The incident angle alpha is ranged from 0 degrees to 45 degrees and the reduced velocity V-r is ranged from 3 to 14. The effects of incident angle and reduced velocity on the dynamic responses and wake flow patterns behind four cylinders are investigated. The results show that the incident angle has a significant effect on the vibration amplitudes and force coefficients of four cylinders, especially for the downstream cylinders, where the maximum vibration amplitudes and force coefficients are occurred mostly on the downstream cylinder. With increasing of the incident angle alpha, the orbital trajectory for each cylinder becomes irregular and complicated, especially at high reduced velocities V-r = 8, corresponding to multiple oscillation frequencies. Moreover, the wake flow patterns behind four cylinders are modified significantly with variations of incident angles, accompanied by different vortex shedding modes.
机译:本文提出了在低雷诺数Re = 150和质量比为2.0的情况下,四个弹性安装的方形圆柱体在两自由度涡激振动的数值研究。入射角α的范围是0度到45度,降低的速度V-r的范围是3到14。研究了入射角和降低的速度对四个圆柱体后面的动力响应和尾流模式的影响。结果表明,入射角对四个气缸的振动幅度和力系数有显着影响,特别是对于下游气缸,最大振动幅度和力系数主要发生在下游气缸上。随着入射角α的增加,每个圆柱体的轨道轨迹变得不规则和复杂,尤其是在高降低速度V-r> = 8时,对应于多个振荡频率。此外,随着入射角的变化,伴随着不同的涡旋脱落模式,四个汽缸后面的尾流模式被显着改变。

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